Premix burner with high flame stability having a net-like structure within the mixing section
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F02C-001/00
F02G-003/00
출원번호
US-0199058
(2002-07-22)
우선권정보
DE-0036313 (2001-07-26); DE-0064097 (2001-12-24)
발명자
/ 주소
Griffin, Timothy
Jansohn, Peter
Ruck, Thomas
출원인 / 주소
Alstom Technology LTD
대리인 / 주소
Burns, Doane, Swecker & Mathis, L.L.P.
인용정보
피인용 횟수 :
9인용 특허 :
9
초록▼
The invention relates to a premix burner with high flame stability for use in a heat generator, preferably in the combustion chamber of a gas turbine. Modern, lean-operated premix burners enable very low noxious emissions, but sometimes operate very close to the extinction limit. To increase the sta
The invention relates to a premix burner with high flame stability for use in a heat generator, preferably in the combustion chamber of a gas turbine. Modern, lean-operated premix burners enable very low noxious emissions, but sometimes operate very close to the extinction limit. To increase the stability of the lean premix combustion by increasing the distance between flame temperature and extinction limit temperature the invention proposes to equip the burner in the mixing zone ( 200 ) with a net-like structure ( 201 ) for the premixing of combustion air and fuel. According to a preferred embodiment, the net-like structure ( 201 ) consists of a plurality of layers of individual wire mesh fabrics ( 202 ) arranged at a distance from each other. The wire mesh fabrics ( 202 ) are preferably equipped with an oxidation-promoting, catalytically active surface. It was found that the net structure ( 201 ) positively influences the thermoacoustic behavior of the burner and dampens and insulates pressure waves from the combustion chamber ( 300 ), and in this way reduces the excitation of pressure waves in the combustion chamber ( 300 ).
대표청구항▼
1. Premix burner with high flame stability for use in a heat generator, preferably of a gas turbine, comprising:a swirl generator with means for the tangential feeding in of a combustion air flow into an inner chamber of the swirl generator,means for feeding in at least one fuel into the combustion
1. Premix burner with high flame stability for use in a heat generator, preferably of a gas turbine, comprising:a swirl generator with means for the tangential feeding in of a combustion air flow into an inner chamber of the swirl generator,means for feeding in at least one fuel into the combustion air stream while forming a swirl flow with an axial movement component towards a burner mouth,a mixing section located downstream from the swirl generator for premixing the combustion air with the at least one fuel,a net-like structure arranged within the mixing section and extending at least approximately over an entire flow cross-section of the mixing section,wherein an open sieve surface of the net-like structure increases radially from an inside area to an outside area over the flow cross-section of the mixing section for promoting an edge flow. 2. Premix burner according to claim 1, wherein the net-like structure is composed of one or more individual wire mesh fabrics that are spaced apart from each other. 3. Premix burner according to claim 2, wherein the net-like structure consists of five to 100, preferably 10 to 20, wire mesh fabrics spaced apart from each other and oriented at least approximately vertically to a longitudinal burner axis. 4. Premix burner according to claim 2, wherein the individual wire mesh fabrics are arranged essentially parallel and at even intervals. 5. Premix burner according to claim 7, wherein an axial distance between the individual wire mesh fabrics corresponds to at least a wire thickness. 6. Premix burner according to claim 1, wherein the net-like structure has a mesh width in the range from 250 μm to 1000 μm, and a wire thickness of 100 μm to 500 μm. 7. Premix burner according to claim 1, wherein the net-like structure is a porous body of a foamed metallic material or foamed ceramic material. 8. Premix burner according to claim 1, wherein the net-like structure is arranged close to the outlet geometry of the mixing section. 9. Premix burner according to claim 1, wherein the net-like structure is based on a high temperature-resistant, metallic material. 10. Premix burner according to claim 9, wherein the net-like structure is based on steel alloy. 11. Premix burner according to claim 10, wherein the net-like structure includes an aluminum-containing steel alloy. 12. Premix burner according to claim 1, wherein the net-like structure is based on a ceramic material. 13. Premix burner according to claim 12, wherein the net-like structure is based on silicon, zirconium, or aluminum compound. 14. Premix burner according to claim 1, wherein at least one wire mesh of the net-like structure has a catalytically active surface. 15. Premix burner according to claim 14, wherein the wire mesh includes a steel alloy and has a porous, ceramic coating provided with a catalytic material. 16. Premix burner according to claim 1, wherein a housing surrounding the mixing section is composed of individual lengths of pipe, and one or more layers of wire mesh of the net structure are integrated in a form-derived or force-derived manner into joints between the individual lengths of pipe. 17. Premix burner according to claim 1, wherein the net structure is integrated in an exchangeable length of pipe of a housing surrounding the mixing section. 18. Premix burner according to claim 1, wherein the net-like structure has a ring-shaped edge zone with a larger open sieve surface than the inside area. 19. Premix burner according to claim 18 for operating in a combustion chamber of a gas turbine section.
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이 특허에 인용된 특허 (9)
Feeley Jennifer S. (Clinton NJ) Fu James C. (Plainsboro NJ) Larkin Matthew P. (Cranbury NJ) Simone Dianne O. (Edison NJ), Catalytic combustion system including a separator body.
Dalla Betta Ralph A. ; Schlatter James C. ; Cutrone Martin Bernard ; Beebe Kenneth Winston, Support structure for a catalyst in a combustion reaction chamber.
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